15 DEC 14: Page 21-04 steps 1-3 left and right: 1.5 hours

Clecoed the A-1004-1R nose ribs and the A-1015-1L inboard nose rib to the A-1003-1L spar.  Clecoed the A-1001A-1L nose skin to the lower flange of the A-1003-1L spar.  Layed the A-1009 counterbalance into the nose skin flush with the outboard edge of the skin.  Clecoed the nose skin to the nose ribs and spar:

16 DEC 14: Page 21-04 step 4 left, pg 21-05 steps 1-2, overcoated tank rivets w/ A sealant: 6.8 hours

Match-drilled the most outboard hole and most inboard hole of the nose skin into the counterbalance:

Final drilled #27 the holes in the counterbalance and nose ribs:

Spent the rest of the session overcoating the tank rivets with A-sealant, which is not as thick as the B-sealant.  It is easy to brush over the shop heads:

17 DEC 14: Page 21-04 step 4, pg 21-05 steps 1-3 right, more A-sealant: 5 hours

Match-drilled the most outboard hole and most inboard hole of the nose skin into the counterbalance. Final drilled #27 the holes in the counterbalance and nose ribs.  Attached the counterbalance to the nose ribs with the hardware called out:

Match-drilled the counterbalance along its length using the holes in the leading edge skin as drill guides:

Finished coating the tank shop heads with A-sealant.

18 DEC 14: Page 21-05 steps 3-5 left: 4 hours

Finished match-drilling the left aileron leading edge skin. Final drilled all the holes in the A-710 stiffeners:

Marked and cut all the stiffeners:

19 DEC 14: Page OP38-2 steps 1-2, pg OP38-3 step 1, pg OP38-4 steps 1-3, pg 21-05 step 5: 4 hours

Separated the aileron trim mounting brackets.  Final-drilled the seven 1/8” holes in each trim mounting bracket.  Final-drilled the sixteen 1/8” holes in the aileron trim links.   Separated the trim links.  Aligned the aileron trim actuation assembly with the wing access plate. Match-drilled the four 5/32” holes in the aileron trim actuation assembly into the wing access plate:

Continued to debur all the aileron parts.  Starting to build a collection for priming:

20 DEC 14: Page 21-05 step 5, pg 22-2 step 1-2: 4.75 hours

Finished cutting and deburring stiffeners.  Finished deburring the spar lightening holes:

Finished deburring the 4 aileron skins:

Constructed the flap cradles:

21 DEC 14: Page 20-4 steps 2-3, pg 18-5 step 7, filet sealed tank end ribs: 8 hours

Marked and cut the W-1021B flap gap stiffeners.  Clecoed the stiffeners to the flap gap fairings.  Clecoed the flap gap and aileron gap fairings to the rear spar and top wing skins.  Attached the fuel flange, anti-rotation plate and nutplates to the tank inboard ribs:

Back:

Filet sealed the end ribs of each tank.  Outside:

Inside: